Page 612 - APPLIED PROCESS DESIGN FOR CHEMICAL AND PETROCHEMICAL PLANTS, Volume 1, 3rd Edition
P. 612

A-6.
            578                                 Altitude and Atmospheric Pressures
                                                        -
                                       Altitude above     Tempera-                    Atmospheric
                                         Sea Level         lure•*      Bara  meter*     Pressure
                                                        ---
                                                                     Inches   mm            Kg/sq
                                  Feet*    Miles   Meters*   •f   ·c   Hg  Abs.   Hg  Abs.   PSIA   cm  Abs.
                                -----                   ---  ---  ---
                                   -5000   ---     -1526   77   25   35.58   903.7   17.48   l  .229
                                   -4500   ----    -1373   75   24   35.00   889.0   17 .19   1  .209
                                   -4000   ---     -1220   73   23   34.42   874.3   16.90   l  .188
                                   -3500   ---     -1068   71   22   33.84   859.5   16.62   I  .169
                                   -3000   ---      -915   70   21   33.27   845. I   16.34   I  .149
                                   -2500   ---      -763   68   20   32.70   830.6   16.06   l  .129
                                   -2000   ---      -610   66   19   32 .14   816.4   15.78   1  .109
                                   -1500   --       -458   64   18   31  .58   802. I   15.51   1.091
                                   -1000  ---  '    -305   63   17   31  .02   787.9   15.23   l  .071
                                    -500   ---      -153   61   16   30.47   773.9   14.96   1.052
                                      0   ---         0    59   15   29.92   760.0   14.696   l  .0333
                                     500   ---       153   57   14   29.38   746.3   14.43   1.015
                                    1000   ---       305   55   13   28.86   733.0   14 .16   .956
                                    1500   ---       458   54   12   28.33   719.6   13.91   .978
                                    2000   ---       610   52   11   27.82   706.6   13.66   .960
                                    2500   ---       763   50   10   27.32   693.9   13.41   .943
                                    3000   ---       915   48   9   26.82   681  .2   13.17   .926
                                    3500   ---      1068   47   8   26.33   668.8   12.93   .909
                                    4000   ---      1220   45   7   25.84   656.3    12.69   .892
                                    4500   --�--    1373   43   6   25.37   644.4   12.46   .876
                                    5000   0.95     1526   41   5   24.90   632.5   12.23   .860
                                    6000    1.1     1831   38   3   23.99   609.3   11 .78   .828
                                    7000    1.3     2136   34   1   23. 10   586.7   11  .34   .797
                                    8000    1  .5   2441   31   -1   22.23   564.6   10.91   .767
                                    9000    1  .7   2746   27   -3   21  .39   543.3   10.50   .738
                                   10,000   1.9     3050   23   -5   20.58   522.7   10.10   .710
                                   15,000   2.8     4577   6  -14   16.89   429.0    8.29   .583
                                   20,000   3.8     6102   -12   -24   13.76   349.5   6.76   .475
                                   25,000   4.7     7628   -30   -34   11  .12   282.4   5.46   .384
                                   30,000   5.7     9153   -48   -44   8.903   226.1   4.37   .307
                                   35,000   6.6    10,679   -66     7.060   179.3    3 .47   .244
                                   40,000   7.6    12,204   -70   -57   5.558   141 .2   2 .73   .192
                                   45,000   8.5    13,730   -70  -57   4.375   111  .  l   2 .15   .151
                                   50,000   9.5    15,255   -70   -57   3.444   87.5   1.69   .  119
                                   55,000   10 .4   16,781   -70  -57   2 .712   68.9   l  .33   .0935
                                   60,000   11.4   18,306   -70   -57   2 .135   54.2   1.05   .0738
                                   70,000   13.3   21,357   -67   -55   1  .325   33.7   .651   .0458
                                   80,000   15.2   24,408   -62   -52   ts .213- 1   21  .0   .406   .0285
                                   90,000   17.1   27,459   -57  -59   5  .200-1   13.2   .255   .0179
                                  100,000   18.9   30,510   -51   -46   3 .290- 1   8.36   .  162   .0114
                                  120,000   22.8   36,612   -26   -48   1  ,359-1   3 .45
                                  140,000   26.6   42,714   4  -16   5. 947-1   I.SI
                                  160,000   30.4   48,816   28   -2   2  .746-2   te , 97- 1
                                  180,000   34 .2   54,918   19   -7   1  .294- 2   3 .26-1
                                  200,000   37.9   61,020   -3   -19   5  .846-J   l  .48-1
                                  220,000   41  .7   67,122   -44  -42   2.  523-3   6  .41- 2
                                  240,000   45.5   73,224   -·86   --66   9.  955-4   2 _53- 2
                                  260,000   49  .3   79,326   -129   -90   !   3 .513-4   8 .92-J
                                  280,000   53. l   85,428  -135   -93   1.  143-4   3 .67-3
                                  300,000   56.9   91,530   -127   --88   3 ,737-s   9  _49- 4
                                  400,000   75.9   122,040   --  ·-   6  _3- 7   l  .60-s
                                  500,000   94.8   152,550   -·-  --   l  .  4- 7   3. 56-6
                                  600,000   I  14   183,060   i--·   -·-   5. 9-•   1  .50- 6
                                  800,000   152   244,080  --  --   1  .6-·   4.  06- 7
                                 1,000,000   189   305,100   --  -   5. J-9   1  . 30-1
                                 I ,200,000   228   366,120  --  -   2 .0- 9   s .os-«
                                 I ,400,000   I   266   427, l 40  --  --   s.2- 10   2 .09-,
                                 1,600,000  .  304   488,160  --  --   3 _9-10   9 .65-•
                                 1,800,000   342   549,180   --  ---   1  _9-10   4. 57-,
                                 2,000,000  '  379   610,200   --  --   I   9.2- 11   2  ,34- 9
                                         '
                                         I                        ;
                                                                                       -----
                                   Data  from  NASA  Standard  Atmosphere  (1962).
                                  *Temperature  and  barometer are  approximate  for negative  altitudes.
                                 **Temperatures  are  average  existing  at  40°  latitude  and  are  rounded  to  even  numbers.
                                  tNegative  exponent shows  number  of spaces  the  decimal  point  must  be  moved  to  the left,
                                   Courtesy Ingersoll-Rand Co.
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